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Computer models and output, Spartan REM: Appendix BA computer model of the Spartan Release Engagement Mechanism (REM) is presented in a series of numerical charts and engineering drawings. A crack growth analysis code is used to predict the fracture mechanics of critical components.
Document ID
19850003068
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Marlowe, D. S. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
West, E. J. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
June 19, 1984
Subject Category
Structural Mechanics
Report/Patent Number
LMSC-HREC-PR-D951498-B
NAS 1.26:171093
NASA-CR-171093
Report Number: LMSC-HREC-PR-D951498-B
Report Number: NAS 1.26:171093
Report Number: NASA-CR-171093
Accession Number
85N11376
Funding Number(s)
CONTRACT_GRANT: NAS8-35599
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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